IntelsatElevenElementsPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total6 of 42698%0 of 0n/a216266216
getMass(AbsoluteDate)30%n/a111111
getFrame()30%n/a111111
propagateInEcef(AbsoluteDate)147100%n/a0102501
computeSatelliteEastLongitudeDegrees(UnivariateDerivative2, FieldSinCos, FieldSinCos)93100%n/a010901
computeSatelliteRadiusKilometers(double, FieldSinCos)43100%n/a010601
IntelsatElevenElementsPropagator(IntelsatElevenElements, Frame, Frame, AttitudeProvider, double)40100%n/a0101001
computeSatelliteGeocentricLatitudeDegrees(UnivariateDerivative2, FieldSinCos)34100%n/a010301
propagateOrbit(AbsoluteDate)18100%n/a010101
IntelsatElevenElementsPropagator(IntelsatElevenElements)10100%n/a010201
IntelsatElevenElementsPropagator(IntelsatElevenElements, Frame, Frame)9100%n/a010201
resetInitialState(SpacecraftState)7100%n/a010101
resetIntermediateState(SpacecraftState, boolean)7100%n/a010101
getEastLongitudeDegrees()3100%n/a010101
getGeocentricLatitudeDegrees()3100%n/a010101
getOrbitRadius()3100%n/a010101
getIntelsatElevenElements()3100%n/a010101